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#101
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Even cars that come off the assembly line the same day all drive different, so all planes will fly different as well, especially the ones that were hand made or used different materials.
So even if you have flown a real Spit, you have flown an unique example with unique characteristics. Imagine each time you fly a plane it has randomly generated characteristics (within the range of the specifications, obviously). That will teach people to be cautious in seeking it's limitations. |
#102
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Why? I thought discussion and debate helped find the truth?
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How condescending. I know a fair bit about trim and a/c having been 6 years in the RAF cadets, flown a glider solo and generally done my research over the years. I've also got a lot of material on The Spitfire, some old, rare books that aren't widely known and therefore quoted. Quote:
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What I mean by this is if your aircraft is trimmed for the slowest regime of flight at max power, and you go diving it to max speed it'll require a helluva lot of force to keep the a/c attitude. Arbitrarily say an a/c has a aileron stick force requirement of 20kg when trimmed out in the middle of her speed range. For arguments sake call it 250mph. That means at lowest, e.g. 100mph that should require 20kg of pressure to, let's say, the right against the torque. Similarly at max speed, say 400mph, that required 20kg of pressure is now to the left to compensate for the inherent trimming of the airframe. Cool. Ok. What happens if we make our datum 175 mph instead? Well down at 100mph against torque we only need 10kg of pressure - however at 400 suddenly you need 30kg of pressure to keep the a/c on keel. It's counter intuitive to me to think that any aircraft that will regularly fly at any of theses speeds would be so set up to give such variance of 300% in trim forces, and although only an example, reflects my attitude regarding the aileron trim modelling. Quote:
He says given the high speeds being reached by 1944, they would have run into aileron reversal had they continued adding more and more power and strengthening the airframe thus pushing it beyond the 450Vne of the airframe, but absolutely NOWHERE does it state that any operational mark of Spitfire suffered from aileron reversal. Last edited by Fenrir; 01-22-2011 at 03:21 PM. |
#103
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That means you don't "know". Is suggest you bring proof for your theories. Why drop a line to Flying heritage? Or, maybe your even able to contact a ret. RAF testpilot. Defending your point of view is much easier if you have something to show which actually backs ups your argument. Edit: Quote:
"Elliptical wing" & "Improved late wing designs" Last edited by swiss; 01-22-2011 at 11:17 AM. |
#104
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TD have made a decision about the aileron neutral trim speed that they interpreted from the manual. Nowhere, nowhere, does it say in that manual, that the max economical cruise speed and rpm is the setting at which the a.c is trimmed. THEY INTERPRETED AND INFERRED IT. On that note, I'm trying to correct it, based on EDUCATED and INFORMED analysis and some RESEARCH. I can't give you a figure but I'm trying to find it and in the meantime, demonstrate the questionable logic of having an a/c - any a/c - trimmed for such a low relative speed in it's performance envelope. |
#105
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Cheers, 6S.Insuber |
#106
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To quote your wiki link: Quote:
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#107
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Fenrir, I which country do you live?
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#108
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Cheers, 6S.Insuber |
#109
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Fenrir, you have informed me greatly goddammit. ![]() |
#110
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